The results of development and manufacture of a micro gas turbine engine for an unmanned aerial vehicle are presented. The calculation features of the main elements of the engine blading section, namely, a centrifugal compressor, a reverse-flow combustor, and a radial-axial turbine are considered. The design of the inlet and output duct, rotor bearings, and lubrication system is described.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Micro Gas Turbine Engine for Unmanned Aerial Vehicles


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 62 , 4 ; 651-660


    Publication date :

    2019-10-01


    Size :

    10 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Micro Gas Turbine Engine for Unmanned Aerial Vehicles

    Sychenkov, V. A. / Limanskii, A. S. / Yousef, W. M. et al. | Online Contents | 2019


    A Heavy-Fueled Engine for Unmanned Aerial Vehicles

    Wood, Charles D. / Boyer, LeMoyne / Gale, Nigel F. et al. | SAE Technical Papers | 1995


    UNMANNED AERIAL VEHICLES

    NUÑEZ FERNANDEZ ALBERTO / HILARIO SERRANO EDUARDO / SERRANO MONTERO CESAR | European Patent Office | 2024

    Free access

    UNMANNED AERIAL VEHICLES

    NUÑEZ FERNANDEZ ALBERTO / HILARIO SERRANO EDUARDO / SERRANO MONTERO CESAR | European Patent Office | 2024

    Free access

    Unmanned Aerial Vehicles

    IAIN MATTHEW RUSSELL | European Patent Office | 2023

    Free access